Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Radial flow devices
Patent
1983-05-27
1986-12-30
Garrett, Robert L.
Fluid reaction surfaces (i.e., impellers)
Specific blade structure
Radial flow devices
416235, 416243, 416DIG2, B63H 126
Patent
active
046326367
ABSTRACT:
A propeller (10) including a hub (12) and a plurality of blades (16) having a leading edge (22), outside edge (24), tail edge (26) and inside edge (28). Each of the blades (16) extend substantially radially from the hub (12) and include a body portion having a regressive pitch from the leading edge (22) to the tail edge (26) and cupped portions (30) and (32) extending along the inside edge (28) and outside edge (24), respectively. A method of making the propeller (10) includes the steps of forming the hub (12) and forming the plurality of blades (16) having a regressive pitch and extending substantially radially from the hub and forming the first cupped portion (30) extending along the inside edge (28) and the second cupped portion (32) extending along the outside edge (24).
REFERENCES:
patent: 535271 (1895-03-01), Armstrong
patent: 1030047 (1912-06-01), Ames
patent: 1582978 (1926-05-01), Grilli
patent: 2754919 (1956-07-01), Blue
patent: 2978040 (1961-04-01), Wirkkala
patent: 3635590 (1972-01-01), Phillips
Garrett Robert L.
Milton Jr. Harold W.
Pitko Joseph M.
Smith Edward H.
LandOfFree
Propeller with blades having regressive pitch does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Propeller with blades having regressive pitch, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Propeller with blades having regressive pitch will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-1544869